SPACE DEBRIS CAPTURE APPARATUS AND METHODS FOR IMPLENTING THE SAME
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United States of America
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Issued Date -
Jan 30, 2025
app pub date -
Jan 11, 2023
filing date -
Jan 11, 2023
priority date (Note) -
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Abstract
A satellite includes a structural element that is deformable during a collision with space object(s). The structural element includes a first side, a second side spaced apart from the first side to define an interior portion between the first side and the second side. and at least one material disposed within the interior portion. The first side includes a first layer of material with payload element(s) disposed thereon, and the second side includes a second layer of material. The material disposed within the interior portion is designed to absorb energy over time during a collision process with each space object. The first layer, the second layer and/or the material disposed within the interior portion are configured to capture one or more space objects upon collision with the satellite.
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